• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-29 09:30来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 - do a check of the wiring between the EIU-1 (1KS1) pin AC/1 and the circuit breaker (3JH1).
 1 If there is no continuity:
_ - repair the above wiring.
 2 If there is continuity:
_
 - replace the C/B-ENGINE/IGN/ENG1/SYS B (3JH1).
 (3) If the fault continues:
 - make sure that there is no ground signal at the EIU-1 (1KS1) pin AA/5B.
 B. If the circuit breaker (3JH1) is open:
 - close it.
 (1) If the circuit breaker trips:
 - remove the ECU (4000KS) (Ref. AMM TASK 73-21-60-000-001)

 - remove the EIU-1 (1KS1) (Ref. AMM TASK 73-25-34-000-040).


 F 『 EEFF : ALL E ∞∞71-50-00∞∞∞∞∞∞∞∞∞∞Page 252
 E E Nov 01/02 E E ECES
E E 56 E E E (2) If the circuit breaker trips again:

 F  『
 E  C F M  E
 E  E

 

 - do a check and repair the wiring for short to ground between the EIU-1 pin AC/1 and the circuit breaker (3JH1).
 (a) If the fault continues:
 - replace the C/B-ENGINE/IGN/ENG1/SYS B (3JH1).
 (3) If the circuit breaker stays closed:
 - install the EIU-1 (1KS1) (Ref. AMM TASK 73-25-34-400-040).
 (a) If the circuit breaker trips:

 - replace the EIU-1 (1KS1) (Ref. AMM TASK 73-25-34-000-040) and (Ref. AMM TASK 73-25-34-400-040).

 (b) If the circuit breaker stays closed:


 - install the ECU (4000KS) (Ref. AMM TASK 73-21-60-400-001).
 1 If the circuit breaker trips:
_
 - replace the ECU (4000KS) (Ref. AMM TASK 73-21-60-000-001) and (Ref. AMM TASK 73-21-60-400-001).
 2 If the circuit breaker trips again:
_
 - do a check and repair the wiring between the ECU (4000KS) pins J2/7, 8 and the EIU-1 pin AC/4.
 (4) If the fault continues:
 - make sure that there is no ground signal at the EIU-1 (1KS1) pin AA/5B.
 C. Do the test given in Para. 3.A.
 F 『 EEFF : ALL E ∞∞71-50-00∞∞∞∞∞∞∞∞∞∞Page 253
 E E Nov 01/02 ERE
ECES E

 F 『
 E C F M E
 E E
 E 56 E
 E E


 TASK 71-50-00-810-827
 Loss of the 115VAC Power Supply on the ECU 2
 1. Possible Causes
_______________
 - EIU-2 (1KS2)

 - ECU (4000KS)

 - J2 harness

 - wiring

 - C/B-ENGINE/ING/ENG2/SYS B (3JH2)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
R AMM 73-21-60-000-001 Removal of the Electronic Control Unit (ECU)(4000KS) AMM 73-21-60-400-001 Installation of the Electronic Control Unit R (ECU)(4000KS) AMM 73-25-34-000-040 Removal of the Engine Interface Unit (EIU) (1KS1,1KS2) AMM 73-25-34-400-040 Installation of the Engine Interface Unit (EIU) (1KS1,1KS2) AMM 73-29-00-710-040 Operational Test of the FADEC on the Ground (with Engine non Motoring) ASM 74-31/01
 3. Fault Confirmation
__________________
 A. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
 -------------------------------------------------------------------------------
121VU ENGINE/IGN/ENG2/SYS B 3JH2 P42
 B. Test
 (1) If you cannot close the circuit breaker (3JH2), refer to Para. 4.B.

 (2) Do the operational test of the FADEC 2B on the ground (with engine non motoring) (Ref. AMM TASK 73-29-00-710-040).


 F 『 EEFF : ALL E ∞∞71-50-00∞∞∞∞∞∞∞∞∞∞Page 254
 E E Aug 01/99 E E ECES
E

 F 『
 E C F M E
 E E
 E 56 E
 E E


 4. Fault Isolation
_______________
 A. If the circuit breaker (3JH2) is closed and if the test gives the maintenance message J2, 115 VAC, ECU:
R  CAUTION : WHEN THE "ENG/MASTER" LEVER IS IN THE "ON" POSITION, BE VERY_______
R  CAREFUL NOT TO SET THE "ENG/MODE" SELECTOR SWITCH TO "CRANK" OR
R  "IGN/START".
R  IF YOU DO SET THE SELECTOR SWITCH TO ONE OF THESE POSITIONS,
R  THE ENGINE WILL START. THERE IS THUS A RISK OF INJURY TO
R  PERSONS AND OF DAMAGE TO EQUIPMENT.
R - On the panel 115 VU, set the MASTER switch to "ON".
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320 Trouble Shooting Manual 排故手册 动力装置 POWER PLANT(26)